Experimental investigations of wall integrated impingement cooling configurations for thermally highly loaded gas turbine blades
Impingement cooling configurations for gas turbine blades
1. Aufl.
2011
XII, 139 S.
210 mm x 148 mm, 247 g
Ill., graph. Darst.
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Digital preservation by Universitätsbibliothek Stuttgart
Theses
German , English
BKL: | 52.30 Strömungskraftmaschinen, Turbomaschinen |
AIAA-2005-1114 FILM COOLING OF HIGHLY LOADED BLADES
British Library Conference Proceedings | 2005
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